tip-leakage flow

基本解释

Upstream stator-rotor interaction reduces the double leakage flow intensity in the rotor tip region.
上游静叶干涉减少了动叶顶部二次泄漏流强度。
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Three-dimensional flow of the tip leakage vortex inside an axial-flow compressor rotor passage was studied using a 3-D Laser Doppler Velocimetry.
用三维激光多普勒测速系统测量了轴流压气机设计状态转子叶尖泄漏涡+和尾迹在静子尖区的传播过程。
In this paper, the influence of tip leakage flow on the 3-D viscous flow field is investigated for different blade tip gap shapes under the condition of rotating hub or stationary hub.
本文针对几种不同形态的叶栅顶部间隙，在环壁转动与静止的不同情况下，研究间隙内的泄漏流动对三维粘性流场的影响。
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